Optimization-Based Aeroengine Nonlinear Control Integration

Aeroengine transient control has been analysed and one of the most important requirements for transient control is the safe and quick response to power request. Theoretically, the optimal operation is to follow the boundary of surge line (with surge margin) for acceleration while decreasing along burner blow-out limit for deceleration. However, in practice, surge and blow-out boundaries are extremely difficult to determine, particularly due to performance drift over flight envelope as well as engine usage cycle.

[1]  Vicenç Torra,et al.  A comparison of active set method and genetic algorithm approaches for learning weighting vectors in some aggregation operators , 2001, Int. J. Intell. Syst..

[2]  Peter J. Fleming,et al.  Fuzzy scheduling control of a gas turbine aero-engine: a multiobjective approach , 2002, IEEE Trans. Ind. Electron..

[3]  Michael Lichtsinder,et al.  Jet Engine Model for Control and Real-Time Simulations , 2006 .

[4]  Philip M. Morse,et al.  Methods of Operations Research , 1952 .

[5]  Wilson J. Rugh,et al.  Stability preserving interpolation methods for the synthesis of gain scheduled controllers , 2000, Autom..

[6]  Link C Jaw,et al.  Aircraft Engine Controls: Design, System Analysis, and Health Monitoring , 2009 .

[7]  Philip E. Gill,et al.  An SQP method for the optimal control of large-scale dynamical systems , 2000 .

[8]  Didier Henrion,et al.  Polynomial LPV synthesis applied to turbofan engines , 2010 .

[9]  Wilson J. Rugh,et al.  Research on gain scheduling , 2000, Autom..

[10]  Zhou Miao.  Component-Level Modeling and Analysis of Aeroengine Based on Matlab/Simulink , 2012 .

[11]  Zhu Gui-ping.  Adaptive fuzzy control based on variable universe and its application to aero engine turbine power generator , 2008 .

[12]  Shi Yan.  Optimum design method of acceleration and deceleration control schedule for gas turbine engine , 2013 .

[13]  S. Støren,et al.  The sequential linear quadratic programming algorithm for solving dynamic optimization problems: a review , 1995 .

[14]  Luc Reberga,et al.  PROGRAMMING AND COMPUTING TOOLS FOR JET ENGINE CONTROL DESIGN , 2005 .

[15]  Jan Dimon Bendtsen,et al.  Bumpless transfer between advanced controllers with applications to power plant control , 2003, 42nd IEEE International Conference on Decision and Control (IEEE Cat. No.03CH37475).

[16]  William Leithead,et al.  Survey of gain-scheduling analysis and design , 2000 .

[17]  Yu Yao,et al.  Linear matrix inequality-based robust h ∞ control of sampled-data systems with parametric uncertainties , 2008 .

[18]  David Q. Mayne,et al.  Constrained model predictive control: Stability and optimality , 2000, Autom..

[19]  Didier Henrion,et al.  LPV MODELING OF A TURBOFAN ENGINE , 2005 .

[20]  Pierre Apkarian,et al.  Self-scheduled H∞ control of linear parameter-varying systems: a design example , 1995, Autom..

[21]  Robert R. Bitmead,et al.  Nonlinear model predictive control of an aircraft gas turbine engine , 2002, Proceedings of the 41st IEEE Conference on Decision and Control, 2002..

[22]  B.P. Rasmussen,et al.  Stable controller interpolation for LPV systems , 2008, 2008 American Control Conference.

[23]  Mark Whittaker,et al.  Shaped metal deposition of a nickel alloy for aero engine applications , 2008 .

[24]  Reinhard Mönig,et al.  Development of Advanced Compressor Airfoils for Heavy-Duty Gas Turbines: Part I — Design and Optimization , 1999 .

[25]  G. G. Kulikov,et al.  On-line performance optimisation of aero engine control system , 2003, Autom..

[26]  Fen Wu,et al.  Induced L2‐norm control for LPV systems with bounded parameter variation rates , 1996 .

[27]  Didier Henrion,et al.  Polynomial LPV synthesis applied to turbofan engines , 2007 .

[28]  H. Maurer,et al.  SQP-methods for solving optimal control problems with control and state constraints: adjoint variables, sensitivity analysis and real-time control , 2000 .

[29]  Didier Henrion,et al.  Linearization and Identification of Aircraft Turbofan Engine Models , 2004 .

[30]  Peter J. Fleming,et al.  Evolutionary algorithms in control systems engineering: a survey , 2002 .

[31]  Andy M. Yip,et al.  A Primal-Dual Active-Set Method for Non-Negativity Constrained Total Variation Deblurring Problems , 2007, IEEE Transactions on Image Processing.

[32]  J. Horlock,et al.  Advanced Gas Turbine Cycles: A Brief Review of Power Generation Thermodynamics , 2013 .

[33]  Jack D. Mattingly,et al.  Aircraft Engine Controls , 2009 .

[34]  F. Bruzelius.  Linear Parameter-Varying Systems - an approach to gain scheduling , 2004 .

[35]  Kai Zheng,et al.  $H_{\infty}$ Bumpless Transfer Under Controller Uncertainty , 2009, IEEE Transactions on Automatic Control.

[36]  Gary J. Balas,et al.  Linear, parameter‐varying control and its application to a turbofan engine , 2002 .

[37]  Ian Postlethwaite,et al.  A switching scheme for full-envelope control of a V/STOL aircraft using LQ bumpless transfer , 2002, Proceedings of the International Conference on Control Applications.

[38]  Shan Wei-wei.  A global optimization approach to aero-engine under transient conditions , 2007 .